Aerospace Systems Laboratory

Shuttle Projects

ISS Projects

LDB Projects

Misc

PEP
WCI
PFMI
SUBSA
DOME
DSTB
Sounding Rocket
KC135

PEP





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WCI







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Pore Formation and Mobility (PFM)

The purpose of the PFM investigation is to promote the understanding of detrimental porosity formation and mobility during controlled directional solidification processing in a microgravity environment. The ultimate goal is required to produce uniformly aligned hypermonotectic composites. The hardware will be launched as stowage in either the orbiter middeck of the Mini-Pressurized Logistics Module (MPLM), and then transferred to stowage on the ISS. The hardware will be operated in the Microgravity Science Glovebox (MSG) and then returned.







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Solidification Using a Baffle in Sealed Ampoules (SUBSA)

The purpose of the SUBSA investigation is to test the performance of an automatically moving baffle in microgravity and to determine the behavior and possible advantages of liquid encapsulation in microgravity conditions. The baffle is used during directional solidification to minimize the natural convection in the melt. The baffle reduces significantly the maximum temperature difference and characteristics size of the melt. In space, the baffle will reduce convection driven by residual acceleration, which is particularly harmful when acting normal to the axis of the ampoule (horizontal Bridgeman growth). This will be investigated by growing Indium Antimonide (InSb) within the SUBSA apparatus, using the Microgravity Science Glovebox (MSG) facility. The hardware will be launched as stowage in either the Orbiter Middeck or in the Mini-Pressurized Logistics Module (MPLM).



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DOME

DOME (Development of Organic Materials for Electronics) is a space flight experiment designed to contribute to the investigation of organic materials based electronic and eletroluminescent devices. A compliment of four vapor deposition chambers fit within a standard NASA Express locker aboard the International Space Station. The compact size also lends itself to ground based vapor deposition applications that have limited resources. The experiment is self-contained, requiring a 28VDC power source and a vacuum-roughing pump. Parameter manipulation such as temperature setpoints and deposition duration is achieved through a standard Ethernet connection.



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DSTB

Test Flight 2005

Data

Download CSV files of data transmitted during Test Flight 0704

Graphs of data transmitted during Test FLight 0704

GPS Data

Pics

Solar Panel Vacuum Chamber Tests

Palestine Pics from Test Flight 0704

Pictures of the baloon launch from Test Flight 0704

Pictures from the AD590 board test

Misc

Map and Directions to Facility


Provided by NSBF

GPS Data for Flight


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Sounding Rocket







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KC135















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Solar Panel Testing

Before deciding on what solar panels to use for the DSTB project, researchers put the panels through a series of tests.

Researchers discussing tests
Researchers discussing tests

The temperature of the panels was an integral part of the test, so the panels were monitored with thermocouples.

Solar Panels with Thermocouples
Solar Panels with Thermocouples

Next the solar panels were placed in a vacuum chamber which has IR lamps to test their performance at high temperatures while in vacuum.

IR Lamp Array On
IR Lamp Array On

Finally the panels were closed up, and the test began.

Vacuum Chamber
Vacuum Chamber

Some panels survived, some did not!

Dead Solar Panel
Dead Solar Panel

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